View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 38222U 12015A 12233.56209491 .00015642 00000-0 14706-3 0 9992
2 38222 051.6428 160.7750 0012821 319.1694 049.9748 15.67244691 19004
| Epoch (UTC): | 20 August 2012 13:29:25 |
| Eccentricity: | 0.0012821 |
| inclination: | 51.6428° |
| perigee height: | 358 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 160.7750° |
| argument of perigee: | 319.1694° |
| revolutions per day: | 15.67244691 |
| mean anomaly at epoch: | 49.9748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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